Modifications of the Turboprop Engine AI-24 for Alternative Energy Application Use.

This work is dedicated to the transformation of aviation turboprop engine AI-24 for energy purposes. The paper provides an analysis of engine construction, design modifications analysis of main components for energy use, as well as analysis of major engine systems. Thermal cycle engine is calculated for first cruise mode. It also discusses the legislative formalities and requirements associated with aircraft engine modifications for energy purposes. The work is also devoted to analysing the actual state of the engine and its inspection. It is a procedure for checking the actual condition of the air turboshaft engine. In the end, it evaluates the use of motor AI-24 for power generation purposes and proposes the possibilities for solving problems of implementation of aircraft turboprop engines for energy purposes. [ABSTRACT FROM AUTHOR]